Low Speed Aerodynamic Wind Tunnel
14
Description
Full scale commercial aircraft fuselage mock-up for wind tunnel testing
Length 20m, weight 6tons
European Project – ARTIC
Deliverables
Design & study of the interface assembly, support frame assembly, Hydraulic lifting mechanism for pitch angle adjustment, main-landing-gear support structure, front and rear endcaps
Engineering drawings in accordance to ASME Y14.5-2009 and DIN 7168-f-R